View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 10515U 26096.92394933 +.00000000 +00000-0 +10402-3 0 00000
2 10515 81.2474 34.6794 0024891 171.4291 188.7309 14.09110812 05
| Epoch (UTC): | 06 April 2026 22:10:29 |
| Eccentricity: | 0.0024891 |
| inclination: | 81.2474° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 34.6794° |
| argument of perigee: | 171.4291° |
| revolutions per day: | 14.09110812 |
| mean anomaly at epoch: | 188.7309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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